View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53736U 26145.08260968 +.00000000 +00000-0 +32168-4 0 00008
2 53736 53.2154 271.3695 0001272 87.5150 272.5987 15.08839956 01
| Epoch (UTC): | 25 May 2026 01:58:57 |
| Eccentricity: | 0.0001272 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 271.3695° |
| argument of perigee: | 87.5150° |
| revolutions per day: | 15.08839956 |
| mean anomaly at epoch: | 272.5987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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